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@ -28,6 +28,7 @@ static double sqr(const double x)
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return x * x;
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}
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// http://williams.best.vwh.net/avform.htm#POINTDME
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double pointsKnownDistanceFromGC(const SGGeoc& a, const SGGeoc&b, const SGGeoc& d, double dist)
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{
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double A = SGGeodesy::courseRad(a, d) - SGGeodesy::courseRad(a, b);
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@ -71,26 +72,559 @@ lat=atan((sin(lat1)*cos(lat2)*sin(lon-lon2)
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return lat;
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}
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RoutePath::RoutePath(const flightgear::WayptVec& wpts) :
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_waypts(wpts)
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static double magVarFor(const SGGeod& geod)
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{
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double jd = globals->get_time_params()->getJD();
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return sgGetMagVar(geod, jd) * SG_RADIANS_TO_DEGREES;
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}
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class WayptData
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{
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public:
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explicit WayptData(WayptRef w) :
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wpt(w),
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hasEntry(false),
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posValid(false),
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legCourseValid(false),
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turnAngle(0.0),
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turnRadius(0.0),
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pathDistanceM(0.0),
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overflightCompensationAngle(0.0),
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flyOver(w->flag(WPT_OVERFLIGHT))
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{
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}
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void initPass0()
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{
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const std::string& ty(wpt->type());
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if (wpt->flag(WPT_DYNAMIC)) {
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if ((ty == "hdgToAlt") || (ty == "radialIntercept") || (ty == "dmeIntercept")) {
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legCourse = wpt->headingRadialDeg();
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legCourseValid = true;
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}
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// presumtpion is that we always overfly such a waypoint
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if (ty == "hdgToAlt") {
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flyOver = true;
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}
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} else {
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pos = wpt->position();
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posValid = true;
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if ((ty == "runway") || (ty == "hold")) {
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legCourse = wpt->headingRadialDeg();
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legCourseValid = true;
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}
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if (ty == "runway") {
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FGRunway* rwy = static_cast<RunwayWaypt*>(wpt.get())->runway();
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turnExitPos = rwy->end();
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}
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} // of static waypt
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}
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// compute leg courses for all static legs (both ends are fixed)
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void initPass1(const WayptData& previous, WayptData* next)
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{
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if (wpt->type() == "vectors") {
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// relying on the fact vectors will be followed by a static fix/wpt
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if (next && next->posValid) {
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posValid = true;
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pos = next->pos;
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}
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}
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if (posValid && !legCourseValid && previous.posValid) {
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// we can compute leg course now
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legCourse = SGGeodesy::courseDeg(previous.pos, pos);
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legCourseValid = true;
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}
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}
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void computeTurn(double radiusM, const WayptData& previous, const WayptData& next)
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{
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assert(legCourseValid && next.legCourseValid);
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turnAngle = next.legCourse - legCourse;
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SG_NORMALIZE_RANGE(turnAngle, -180.0, 180.0);
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turnRadius = radiusM;
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double p = copysign(90.0, turnAngle);
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if (flyOver) {
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turnEntryPos = pos;
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turnCenter = SGGeodesy::direct(pos, legCourse + p, turnRadius);
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// use the leg course
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turnExitPos = SGGeodesy::direct(turnCenter, next.legCourse - p, turnRadius);
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if (!next.wpt->flag(WPT_DYNAMIC)) {
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// distance perpendicular to next leg course, after turning
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// through turnAngle
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double xtk = turnRadius * (1 - cos(turnAngle * SG_DEGREES_TO_RADIANS));
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// compensation angle to turn back on course
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double theta = acos((turnRadius - (xtk * 0.5)) / turnRadius) * SG_RADIANS_TO_DEGREES;
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theta = copysign(theta, turnAngle);
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turnAngle += theta;
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// move by the distance to compensate
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double d = turnRadius * 2.0 * sin(theta * SG_DEGREES_TO_RADIANS);
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turnExitPos = SGGeodesy::direct(turnExitPos, next.legCourse, d);
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overflightCompensationAngle = -theta;
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}
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} else {
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hasEntry = true;
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double halfAngle = turnAngle * 0.5;
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double turnCenterOffset = turnRadius / cos(halfAngle * SG_DEGREES_TO_RADIANS);
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turnCenter = SGGeodesy::direct(pos, legCourse + halfAngle + p, turnCenterOffset);
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double entryExitDistanceAlongPath = turnRadius * tan(fabs(halfAngle) * SG_DEGREES_TO_RADIANS);
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turnEntryPos = SGGeodesy::direct(pos, legCourse, -entryExitDistanceAlongPath);
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turnExitPos = SGGeodesy::direct(pos, next.legCourse, entryExitDistanceAlongPath);
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}
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}
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double turnDistanceM() const
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{
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return (fabs(turnAngle * SG_DEGREES_TO_RADIANS) / SG_PI * 2.0) * turnRadius;
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}
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void turnEntryPath(SGGeodVec& path) const
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{
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assert(!flyOver);
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if (fabs(turnAngle) < 0.5 ) {
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path.push_back(pos);
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return;
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}
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double halfAngle = turnAngle * 0.5;
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int steps = std::max(SGMiscd::roundToInt(fabs(halfAngle) / 3.0), 1);
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double stepIncrement = halfAngle / steps;
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double h = legCourse;
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SGGeod p = turnEntryPos;
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double stepDist = (fabs(stepIncrement) / 360.0) * SGMiscd::twopi() * turnRadius;
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for (int s=0; s<steps; ++s) {
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path.push_back(p);
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p = SGGeodesy::direct(p, h, stepDist);
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h += stepIncrement;
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}
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path.push_back(p);
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}
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void turnExitPath(SGGeodVec& path) const
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{
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if (fabs(turnAngle) < 0.5) {
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path.push_back(turnExitPos);
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return;
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}
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double t = flyOver ? turnAngle : turnAngle * 0.5;
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int steps = std::max(SGMiscd::roundToInt(fabs(t) / 3.0), 1);
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double stepIncrement = t / steps;
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// initial exit heading
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double h = legCourse + (flyOver ? 0.0 : (turnAngle * 0.5));
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double turnDirOffset = copysign(90.0, turnAngle);
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// compute the first point on the exit path. Depends on fly-over vs fly-by
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SGGeod p = flyOver ? pos : SGGeodesy::direct(turnCenter, h + turnDirOffset, -turnRadius);
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double stepDist = (fabs(stepIncrement) / 360.0) * SGMiscd::twopi() * turnRadius;
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for (int s=0; s<steps; ++s) {
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path.push_back(p);
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p = SGGeodesy::direct(p, h, stepDist);
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h += stepIncrement;
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}
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if (flyOver) {
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// skew by compensation angle back
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steps = std::max(SGMiscd::roundToInt(fabs(overflightCompensationAngle) / 3.0), 1);
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// step in opposite direction to the turn angle to swing back onto
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// the next leg course
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stepIncrement = overflightCompensationAngle / steps;
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for (int s=0; s<steps; ++s) {
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path.push_back(p);
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p = SGGeodesy::direct(p, h, stepDist);
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h += stepIncrement;
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}
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}
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path.push_back(p);
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}
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WayptRef wpt;
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bool hasEntry, posValid, legCourseValid;
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SGGeod pos, turnEntryPos, turnExitPos, turnCenter;
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double turnAngle, turnRadius, legCourse;
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double pathDistanceM;
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double overflightCompensationAngle;
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bool flyOver;
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};
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typedef std::vector<WayptData> WayptDataVec;
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class PerformanceBracket
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{
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public:
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PerformanceBracket(double atOrBelow, double climb, double descent, double speed, bool isMach = false) :
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atOrBelowAltitudeFt(atOrBelow),
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climbRateFPM(climb),
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descentRateFPM(descent),
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speedIASOrMach(speed),
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speedIsMach(isMach)
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{ }
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double atOrBelowAltitudeFt;
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double climbRateFPM;
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double descentRateFPM;
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double speedIASOrMach;
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bool speedIsMach;
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};
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typedef std::vector<PerformanceBracket> PerformanceBracketVec;
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bool isDescentWaypoint(const WayptRef& wpt)
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{
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return (wpt->flag(WPT_APPROACH) && !wpt->flag(WPT_MISS)) || wpt->flag(WPT_ARRIVAL);
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}
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class RoutePath::RoutePathPrivate
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{
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public:
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WayptDataVec waypoints;
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PerformanceBracketVec perf;
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PerformanceBracketVec::const_iterator
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findPerformanceBracket(double altFt) const
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{
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PerformanceBracketVec::const_iterator r;
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PerformanceBracketVec::const_iterator result = perf.begin();
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for (r = perf.begin(); r != perf.end(); ++r) {
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if (r->atOrBelowAltitudeFt > altFt) {
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break;
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}
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result = r;
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} // of brackets iteration
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return result;
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}
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void computeDynamicPosition(int index)
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{
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const WayptData& previous(waypoints[index-1]);
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WayptRef wpt = waypoints[index].wpt;
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assert(previous.posValid);
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const std::string& ty(wpt->type());
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if (ty == "hdgToAlt") {
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HeadingToAltitude* h = (HeadingToAltitude*) wpt.get();
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double altFt = computeVNAVAltitudeFt(index - 1);
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double altChange = h->altitudeFt() - altFt;
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PerformanceBracketVec::const_iterator it = findPerformanceBracket(altFt);
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double speedMSec = groundSpeedForAltitude(altFt) * SG_KT_TO_MPS;
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double timeToChangeSec;
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if (isDescentWaypoint(wpt)) {
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timeToChangeSec = (altChange / it->descentRateFPM) * 60.0;
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} else {
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timeToChangeSec = (altChange / it->climbRateFPM) * 60.0;
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}
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double distanceM = timeToChangeSec * speedMSec;
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double hdg = h->headingDegMagnetic() + magVarFor(previous.pos);
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waypoints[index].pos = SGGeodesy::direct(previous.turnExitPos, hdg, distanceM);
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waypoints[index].posValid = true;
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} else if (ty == "radialIntercept") {
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// start from previous.turnExit
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RadialIntercept* i = (RadialIntercept*) wpt.get();
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SGGeoc prevGc = SGGeoc::fromGeod(previous.turnExitPos);
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SGGeoc navid = SGGeoc::fromGeod(wpt->position());
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SGGeoc rGc;
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double magVar = magVarFor(previous.pos);
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double radial = i->radialDegMagnetic() + magVar;
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double track = i->courseDegMagnetic() + magVar;
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bool ok = geocRadialIntersection(prevGc, track, navid, radial, rGc);
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if (!ok) {
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SG_LOG(SG_NAVAID, SG_WARN, "couldn't compute interception for radial:"
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<< previous.turnExitPos << " / " << track << "/" << wpt->position()
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<< "/" << radial);
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waypoints[index].pos = wpt->position(); // horrible fallback
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} else {
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waypoints[index].pos = SGGeod::fromGeoc(rGc);
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}
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waypoints[index].posValid = true;
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} else if (ty == "dmeIntercept") {
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DMEIntercept* di = (DMEIntercept*) wpt.get();
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SGGeoc prevGc = SGGeoc::fromGeod(previous.turnExitPos);
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SGGeoc navid = SGGeoc::fromGeod(wpt->position());
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double distRad = di->dmeDistanceNm() * SG_NM_TO_RAD;
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SGGeoc rGc;
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SGGeoc bPt;
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double crs = di->courseDegMagnetic() + magVarFor(wpt->position());
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|
|
SGGeodesy::advanceRadM(prevGc, crs, 100 * SG_NM_TO_RAD, bPt);
|
|
|
|
|
|
|
|
|
|
double dNm = pointsKnownDistanceFromGC(prevGc, bPt, navid, distRad);
|
|
|
|
|
if (dNm < 0.0) {
|
|
|
|
|
SG_LOG(SG_NAVAID, SG_WARN, "dmeIntercept failed");
|
|
|
|
|
waypoints[index].pos = wpt->position(); // horrible fallback
|
|
|
|
|
} else {
|
|
|
|
|
waypoints[index].pos = SGGeodesy::direct(previous.turnExitPos, crs, dNm * SG_NM_TO_METER);
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
waypoints[index].posValid = true;
|
|
|
|
|
} else if (ty == "vectors") {
|
|
|
|
|
waypoints[index].legCourse = SGGeodesy::courseDeg(previous.turnExitPos, waypoints[index].pos);
|
|
|
|
|
waypoints[index].legCourseValid = true;
|
|
|
|
|
// no turn data
|
|
|
|
|
}
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
double computeVNAVAltitudeFt(int index)
|
|
|
|
|
{
|
|
|
|
|
WayptRef w = waypoints[index].wpt;
|
|
|
|
|
if ((w->flag(WPT_APPROACH) && !w->flag(WPT_MISS)) || w->flag(WPT_ARRIVAL)) {
|
|
|
|
|
// descent
|
|
|
|
|
int next = findNextKnownAltitude(index);
|
|
|
|
|
if (next < 0) {
|
|
|
|
|
return 0.0;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
double fixedAlt = altitudeForIndex(next);
|
|
|
|
|
double distanceM = distanceBetweenIndices(index, next);
|
|
|
|
|
double speedMSec = groundSpeedForAltitude(fixedAlt) * SG_KT_TO_MPS;
|
|
|
|
|
double minutes = (distanceM / speedMSec) / 60.0;
|
|
|
|
|
|
|
|
|
|
PerformanceBracketVec::const_iterator it = findPerformanceBracket(fixedAlt);
|
|
|
|
|
return fixedAlt + (it->descentRateFPM * minutes);
|
|
|
|
|
|
|
|
|
|
} else {
|
|
|
|
|
// climb
|
|
|
|
|
int prev = findPreceedingKnownAltitude(index);
|
|
|
|
|
if (prev < 0) {
|
|
|
|
|
return 0.0;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
double fixedAlt = altitudeForIndex(prev);
|
|
|
|
|
double distanceM = distanceBetweenIndices(prev, index);
|
|
|
|
|
double speedMSec = groundSpeedForAltitude(fixedAlt) * SG_KT_TO_MPS;
|
|
|
|
|
double minutes = (distanceM / speedMSec) / 60.0;
|
|
|
|
|
|
|
|
|
|
PerformanceBracketVec::const_iterator it = findPerformanceBracket(fixedAlt);
|
|
|
|
|
return fixedAlt + (it->climbRateFPM * minutes);
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
int findPreceedingKnownAltitude(int index) const
|
|
|
|
|
{
|
|
|
|
|
const WayptData& w(waypoints[index]);
|
|
|
|
|
if (w.wpt->altitudeRestriction() == RESTRICT_AT) {
|
|
|
|
|
return index;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
// principal base case is runways.
|
|
|
|
|
const std::string& ty(w.wpt->type());
|
|
|
|
|
if (ty == "runway") {
|
|
|
|
|
return index; // runway always has a known elevation
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
if (index == 0) {
|
|
|
|
|
SG_LOG(SG_NAVAID, SG_WARN, "findPreceedingKnownAltitude: no preceeding altitude value found");
|
|
|
|
|
return -1;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
// recurse earlier in the route
|
|
|
|
|
return findPreceedingKnownAltitude(index - 1);
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
int findNextKnownAltitude(int index) const
|
|
|
|
|
{
|
|
|
|
|
if (index >= waypoints.size()) {
|
|
|
|
|
SG_LOG(SG_NAVAID, SG_WARN, "findNextKnownAltitude: no next altitude value found");
|
|
|
|
|
return -1;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
const WayptData& w(waypoints[index]);
|
|
|
|
|
if (w.wpt->altitudeRestriction() == RESTRICT_AT) {
|
|
|
|
|
return index;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
// principal base case is runways.
|
|
|
|
|
const std::string& ty(w.wpt->type());
|
|
|
|
|
if (ty == "runway") {
|
|
|
|
|
return index; // runway always has a known elevation
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
if (index == waypoints.size() - 1) {
|
|
|
|
|
SG_LOG(SG_NAVAID, SG_WARN, "findNextKnownAltitude: no next altitude value found");
|
|
|
|
|
return -1;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
return findNextKnownAltitude(index + 1);
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
double altitudeForIndex(int index) const
|
|
|
|
|
{
|
|
|
|
|
const WayptData& w(waypoints[index]);
|
|
|
|
|
if (w.wpt->altitudeRestriction() != RESTRICT_NONE) {
|
|
|
|
|
return w.wpt->altitudeFt();
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
const std::string& ty(w.wpt->type());
|
|
|
|
|
if (ty == "runway") {
|
|
|
|
|
FGRunway* rwy = static_cast<RunwayWaypt*>(w.wpt.get())->runway();
|
|
|
|
|
return rwy->threshold().getElevationFt();
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
SG_LOG(SG_NAVAID, SG_WARN, "altitudeForIndex: waypoint has no explicit altitude");
|
|
|
|
|
return 0.0;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
double groundSpeedForAltitude(double altitude) const
|
|
|
|
|
{
|
|
|
|
|
// FIXME
|
|
|
|
|
#if 0
|
|
|
|
|
if (0) {
|
|
|
|
|
PerformanceBracketVec::const_iterator it = findPerformanceBracket(altitude);
|
|
|
|
|
double mach;
|
|
|
|
|
|
|
|
|
|
if (it->speedIsMach) {
|
|
|
|
|
mach = it->speedIASOrMach; // easy
|
|
|
|
|
} else {
|
|
|
|
|
const double Cs_0 = 661.4786; // speed of sound at sea level, knots
|
|
|
|
|
const double P_0 = 29.92126;
|
|
|
|
|
const double P = P_0 * pow(, );
|
|
|
|
|
// convert IAS (which we will treat as CAS) to Mach based on altitude
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
double oatK;
|
|
|
|
|
double Cs = sqrt(SG_gamma * SG_R_m2_p_s2_p_K * oatK);
|
|
|
|
|
|
|
|
|
|
double tas = mach * Cs;
|
|
|
|
|
|
|
|
|
|
#if 0
|
|
|
|
|
P_0= 29.92126 "Hg = 1013.25 mB = 2116.2166 lbs/ft^2
|
|
|
|
|
P= P_0*(1-6.8755856*10^-6*PA)^5.2558797, pressure altitude, PA<36,089.24ft
|
|
|
|
|
CS= 38.967854*sqrt(T+273.15) where T is the (static/true) OAT in Celsius.
|
|
|
|
|
|
|
|
|
|
DP=P_0*((1 + 0.2*(IAS/CS_0)^2)^3.5 -1)
|
|
|
|
|
M=(5*( (DP/P + 1)^(2/7) -1) )^0.5 (*)
|
|
|
|
|
TAS= M*CS
|
|
|
|
|
#endif
|
|
|
|
|
}
|
|
|
|
|
#endif
|
|
|
|
|
|
|
|
|
|
return 250.0;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
double distanceBetweenIndices(int from, int to) const
|
|
|
|
|
{
|
|
|
|
|
double total = 0.0;
|
|
|
|
|
|
|
|
|
|
for (int i=from+1; i<= to; ++i) {
|
|
|
|
|
total += waypoints[i].pathDistanceM;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
return total;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
void initPerfData()
|
|
|
|
|
{
|
|
|
|
|
// assume category C/D aircraft for now
|
|
|
|
|
perf.push_back(PerformanceBracket(4000, 1800, 1800, 180));
|
|
|
|
|
perf.push_back(PerformanceBracket(10000, 1800, 1800, 230));
|
|
|
|
|
perf.push_back(PerformanceBracket(18000, 1200, 1800, 270));
|
|
|
|
|
perf.push_back(PerformanceBracket(60000, 800, 1200, 0.85, true /* is Mach */));
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
}; // of RoutePathPrivate class
|
|
|
|
|
|
|
|
|
|
RoutePath::RoutePath(const flightgear::WayptVec& wpts) :
|
|
|
|
|
d(new RoutePathPrivate)
|
|
|
|
|
{
|
|
|
|
|
WayptVec::const_iterator it;
|
|
|
|
|
for (it = wpts.begin(); it != wpts.end(); ++it) {
|
|
|
|
|
d->waypoints.push_back(WayptData(*it));
|
|
|
|
|
}
|
|
|
|
|
commonInit();
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
RoutePath::RoutePath(const flightgear::FlightPlan* fp)
|
|
|
|
|
RoutePath::RoutePath(const flightgear::FlightPlan* fp) :
|
|
|
|
|
d(new RoutePathPrivate)
|
|
|
|
|
{
|
|
|
|
|
for (int l=0; l<fp->numLegs(); ++l) {
|
|
|
|
|
_waypts.push_back(fp->legAtIndex(l)->waypoint());
|
|
|
|
|
d->waypoints.push_back(WayptData(fp->legAtIndex(l)->waypoint()));
|
|
|
|
|
}
|
|
|
|
|
commonInit();
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
void RoutePath::commonInit()
|
|
|
|
|
{
|
|
|
|
|
_pathClimbFPM = 1200;
|
|
|
|
|
_pathDescentFPM = 800;
|
|
|
|
|
_pathIAS = 190;
|
|
|
|
|
_pathTurnRate = 3.0; // 3 deg/sec = 180def/min = standard rate turn
|
|
|
|
|
_pathTurnRate = 3.0; // 3 deg/sec = 180deg/min = standard rate turn
|
|
|
|
|
|
|
|
|
|
d->initPerfData();
|
|
|
|
|
|
|
|
|
|
WayptDataVec::iterator it;
|
|
|
|
|
for (it = d->waypoints.begin(); it != d->waypoints.end(); ++it) {
|
|
|
|
|
it->initPass0();
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
for (unsigned int i=1; i<d->waypoints.size(); ++i) {
|
|
|
|
|
WayptData* nextPtr = ((i + 1) < d->waypoints.size()) ? &d->waypoints[i+1] : 0;
|
|
|
|
|
d->waypoints[i].initPass1(d->waypoints[i-1], nextPtr);
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
for (unsigned int i=1; i<d->waypoints.size(); ++i) {
|
|
|
|
|
d->computeDynamicPosition(i);
|
|
|
|
|
|
|
|
|
|
const WayptData& prev(d->waypoints[i-1]);
|
|
|
|
|
|
|
|
|
|
double alt = 0.0; // FIXME
|
|
|
|
|
double gs = d->groundSpeedForAltitude(alt);
|
|
|
|
|
double radiusM = ((360.0 / _pathTurnRate) * gs * SG_KT_TO_MPS) / SGMiscd::twopi();
|
|
|
|
|
|
|
|
|
|
if (i < (d->waypoints.size() - 1)) {
|
|
|
|
|
WayptData& next(d->waypoints[i+1]);
|
|
|
|
|
if (!next.legCourseValid && next.posValid) {
|
|
|
|
|
// compute leg course now our own position is valid
|
|
|
|
|
next.legCourse = SGGeodesy::courseDeg(d->waypoints[i].pos, next.pos);
|
|
|
|
|
next.legCourseValid = true;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
if (next.legCourseValid) {
|
|
|
|
|
d->waypoints[i].computeTurn(radiusM, prev, next);
|
|
|
|
|
} else {
|
|
|
|
|
// next waypoint has indeterminate course. Let's create a sharp turn
|
|
|
|
|
// this can happen when the following point is ATC vectors, for example.
|
|
|
|
|
d->waypoints[i].turnEntryPos = d->waypoints[i].pos;
|
|
|
|
|
d->waypoints[i].turnExitPos = d->waypoints[i].pos;
|
|
|
|
|
}
|
|
|
|
|
} else {
|
|
|
|
|
// final waypt, fix up some data
|
|
|
|
|
d->waypoints[i].turnEntryPos = d->waypoints[i].pos;
|
|
|
|
|
d->waypoints[i].turnExitPos = d->waypoints[i].pos;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
// now turn is computed, can resolve distances
|
|
|
|
|
d->waypoints[i].pathDistanceM = computeDistanceForIndex(i);
|
|
|
|
|
}
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
SGGeodVec RoutePath::pathForIndex(int index) const
|
|
|
|
@ -99,24 +633,21 @@ SGGeodVec RoutePath::pathForIndex(int index) const
|
|
|
|
|
return SGGeodVec(); // no path for first waypoint
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
if (_waypts[index]->type() == "vectors") {
|
|
|
|
|
const WayptData& w(d->waypoints[index]);
|
|
|
|
|
const std::string& ty(w.wpt->type());
|
|
|
|
|
if (ty == "vectors") {
|
|
|
|
|
return SGGeodVec(); // empty
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
if (_waypts[index]->type() == "hold") {
|
|
|
|
|
return pathForHold((Hold*) _waypts[index].get());
|
|
|
|
|
if (ty== "hold") {
|
|
|
|
|
return pathForHold((Hold*) d->waypoints[index].wpt.get());
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
SGGeodVec r;
|
|
|
|
|
SGGeod from, to;
|
|
|
|
|
if (!computedPositionForIndex(index-1, from)) {
|
|
|
|
|
return SGGeodVec();
|
|
|
|
|
}
|
|
|
|
|
d->waypoints[index - 1].turnExitPath(r);
|
|
|
|
|
|
|
|
|
|
r.push_back(from);
|
|
|
|
|
if (!computedPositionForIndex(index, to)) {
|
|
|
|
|
return SGGeodVec();
|
|
|
|
|
}
|
|
|
|
|
SGGeod from = d->waypoints[index - 1].turnExitPos,
|
|
|
|
|
to = w.turnEntryPos;
|
|
|
|
|
|
|
|
|
|
// compute rounding offset, we want to round towards the direction of travel
|
|
|
|
|
// which depends on the east/west sign of the longitude change
|
|
|
|
@ -125,12 +656,17 @@ SGGeodVec RoutePath::pathForIndex(int index) const
|
|
|
|
|
interpolateGreatCircle(from, to, r);
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
r.push_back(to);
|
|
|
|
|
if (w.flyOver) {
|
|
|
|
|
r.push_back(w.pos);
|
|
|
|
|
} else {
|
|
|
|
|
// flyBy
|
|
|
|
|
w.turnEntryPath(r);
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
if (_waypts[index]->type() == "runway") {
|
|
|
|
|
if (ty == "runway") {
|
|
|
|
|
// runways get an extra point, at the end. this is particularly
|
|
|
|
|
// important so missed approach segments draw correctly
|
|
|
|
|
FGRunway* rwy = static_cast<RunwayWaypt*>(_waypts[index].get())->runway();
|
|
|
|
|
FGRunway* rwy = static_cast<RunwayWaypt*>(w.wpt.get())->runway();
|
|
|
|
|
r.push_back(rwy->end());
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
@ -163,13 +699,7 @@ void RoutePath::interpolateGreatCircle(const SGGeod& aFrom, const SGGeod& aTo, S
|
|
|
|
|
|
|
|
|
|
SGGeod RoutePath::positionForIndex(int index) const
|
|
|
|
|
{
|
|
|
|
|
SGGeod r;
|
|
|
|
|
bool ok = computedPositionForIndex(index, r);
|
|
|
|
|
if (!ok) {
|
|
|
|
|
return SGGeod();
|
|
|
|
|
}
|
|
|
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return r;
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return d->waypoints[index].pos;
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|
}
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|
SGGeodVec RoutePath::pathForHold(Hold* hold) const
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@ -177,14 +707,16 @@ SGGeodVec RoutePath::pathForHold(Hold* hold) const
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int turnSteps = 16;
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double hdg = hold->inboundRadial();
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double turnDelta = 180.0 / turnSteps;
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double altFt = 0.0; // FIXME
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double gsKts = d->groundSpeedForAltitude(altFt);
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SGGeodVec r;
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double az2;
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double stepTime = turnDelta / _pathTurnRate; // in seconds
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double stepDist = _pathIAS * (stepTime / 3600.0) * SG_NM_TO_METER;
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double stepDist = gsKts * (stepTime / 3600.0) * SG_NM_TO_METER;
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double legDist = hold->isDistance() ?
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hold->timeOrDistance()
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: _pathIAS * (hold->timeOrDistance() / 3600.0);
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: gsKts * (hold->timeOrDistance() / 3600.0);
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legDist *= SG_NM_TO_METER;
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if (hold->isLeftHanded()) {
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@ -210,244 +742,48 @@ SGGeodVec RoutePath::pathForHold(Hold* hold) const
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return r;
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}
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bool RoutePath::computedPositionForIndex(int index, SGGeod& r) const
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{
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if ((index < 0) || (index >= (int) _waypts.size())) {
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throw sg_range_exception("waypt index out of range",
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"RoutePath::computedPositionForIndex");
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}
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WayptRef w = _waypts[index];
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if (!w->flag(WPT_DYNAMIC)) {
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r = w->position();
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return true;
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}
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if (w->type() == "radialIntercept") {
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// radial intersection along track
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SGGeod prev;
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if (!computedPositionForIndex(index - 1, prev)) {
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return false;
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}
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SGGeoc prevGc = SGGeoc::fromGeod(prev);
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SGGeoc navid = SGGeoc::fromGeod(w->position());
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SGGeoc rGc;
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double magVar = magVarFor(prev);
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RadialIntercept* i = (RadialIntercept*) w.get();
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double radial = i->radialDegMagnetic() + magVar;
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double track = i->courseDegMagnetic() + magVar;
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bool ok = geocRadialIntersection(prevGc, track, navid, radial, rGc);
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if (!ok) {
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return false;
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}
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r = SGGeod::fromGeoc(rGc);
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return true;
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} else if (w->type() == "dmeIntercept") {
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// find the point along the DME track, from prev, that is the correct distance
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// from the DME
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SGGeod prev;
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if (!computedPositionForIndex(index - 1, prev)) {
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return false;
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}
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DMEIntercept* di = (DMEIntercept*) w.get();
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SGGeoc prevGc = SGGeoc::fromGeod(prev);
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SGGeoc navid = SGGeoc::fromGeod(w->position());
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double distRad = di->dmeDistanceNm() * SG_NM_TO_RAD;
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SGGeoc rGc;
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SGGeoc bPt;
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double crs = di->courseDegMagnetic() + magVarFor(prev);
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SGGeodesy::advanceRadM(prevGc, crs, 100 * SG_NM_TO_RAD, bPt);
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double dNm = pointsKnownDistanceFromGC(prevGc, bPt, navid, distRad);
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if (dNm < 0.0) {
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return false;
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}
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double az2;
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SGGeodesy::direct(prev, crs, dNm * SG_NM_TO_METER, r, az2);
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return true;
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} else if (w->type() == "hdgToAlt") {
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HeadingToAltitude* h = (HeadingToAltitude*) w.get();
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double climb = h->altitudeFt() - computeAltitudeForIndex(index - 1);
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double d = distanceForClimb(climb);
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SGGeod prevPos;
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|
|
if (!computedPositionForIndex(index - 1, prevPos)) {
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|
return false;
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|
}
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|
|
double hdg = h->headingDegMagnetic() + magVarFor(prevPos);
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|
|
double az2;
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|
SGGeodesy::direct(prevPos, hdg, d * SG_NM_TO_METER, r, az2);
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|
|
return true;
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|
|
} else if (w->type() == "vectors"){
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|
|
// return position of next point (which is presumably static fix/wpt)
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|
|
// however, a missed approach might end with VECTORS, so tolerate that case
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|
|
if (index + 1 >= _waypts.size()) {
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|
|
SG_LOG(SG_NAVAID, SG_INFO, "route ends with VECTORS, no position");
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|
|
return false;
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|
|
}
|
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|
|
WayptRef nextWp = _waypts[index+1];
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|
|
if (nextWp->flag(WPT_DYNAMIC)) {
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|
|
SG_LOG(SG_NAVAID, SG_INFO, "dynamic WP following VECTORS, no position");
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|
|
return false;
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|
|
}
|
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|
|
r = nextWp->position();
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|
|
return true;
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|
|
} else if (w->type() == "hold") {
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|
|
r = w->position();
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|
|
return true;
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|
|
}
|
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|
|
SG_LOG(SG_NAVAID, SG_INFO, "RoutePath::computedPositionForIndex: unhandled type:" << w->type());
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|
|
return false;
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|
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}
|
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|
|
double RoutePath::computeDistanceForIndex(int index) const
|
|
|
|
|
{
|
|
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|
|
if ((index < 0) || (index >= (int) _waypts.size())) {
|
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|
|
if ((index < 0) || (index >= (int) d->waypoints.size())) {
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|
|
throw sg_range_exception("waypt index out of range",
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|
|
|
"RoutePath::computeDistanceForIndex");
|
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|
|
}
|
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|
|
if (index + 1 >= (int) _waypts.size()) {
|
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|
|
// final waypoint, distance is 0
|
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|
|
if (index == 0) {
|
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|
|
// first waypoint, distance is 0
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|
|
return 0.0;
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|
|
}
|
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|
|
WayptRef w = _waypts[index],
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|
|
nextWp = _waypts[index+1];
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|
|
// common case, both waypoints are static
|
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|
|
if (!w->flag(WPT_DYNAMIC) && !nextWp->flag(WPT_DYNAMIC)) {
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|
|
return SGGeodesy::distanceM(w->position(), nextWp->position());
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|
}
|
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|
|
SGGeod wPos, nextPos;
|
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|
|
bool ok = computedPositionForIndex(index, wPos),
|
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|
|
nextOk = computedPositionForIndex(index + 1, nextPos);
|
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|
|
if (ok && nextOk) {
|
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|
|
return SGGeodesy::distanceM(wPos, nextPos);
|
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|
|
}
|
|
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|
|
|
|
|
|
|
SG_LOG(SG_NAVAID, SG_INFO, "RoutePath::computeDistanceForIndex: unhandled arrangement:"
|
|
|
|
|
<< w->type() << " followed by " << nextWp->type());
|
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|
|
|
return 0.0;
|
|
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|
|
}
|
|
|
|
|
|
|
|
|
|
double RoutePath::computeAltitudeForIndex(int index) const
|
|
|
|
|
{
|
|
|
|
|
if ((index < 0) || (index >= (int) _waypts.size())) {
|
|
|
|
|
throw sg_range_exception("waypt index out of range",
|
|
|
|
|
"RoutePath::computeAltitudeForIndex");
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
WayptRef w = _waypts[index];
|
|
|
|
|
if (w->altitudeRestriction() != RESTRICT_NONE) {
|
|
|
|
|
return w->altitudeFt(); // easy!
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
if (w->type() == "runway") {
|
|
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|
|
FGRunway* rwy = static_cast<RunwayWaypt*>(w.get())->runway();
|
|
|
|
|
return rwy->threshold().getElevationFt();
|
|
|
|
|
} else if ((w->type() == "hold") || (w->type() == "vectors")) {
|
|
|
|
|
// pretend we don't change altitude in holds/vectoring
|
|
|
|
|
return computeAltitudeForIndex(index - 1);
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
double prevAlt = computeAltitudeForIndex(index - 1);
|
|
|
|
|
// find distance to previous, and hence climb/descent
|
|
|
|
|
SGGeod pos, prevPos;
|
|
|
|
|
|
|
|
|
|
if (!computedPositionForIndex(index, pos) ||
|
|
|
|
|
!computedPositionForIndex(index - 1, prevPos))
|
|
|
|
|
{
|
|
|
|
|
SG_LOG(SG_NAVAID, SG_WARN, "unable to compute position for waypoints");
|
|
|
|
|
throw sg_range_exception("unable to compute position for waypoints");
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
double d = SGGeodesy::distanceNm(prevPos, pos);
|
|
|
|
|
double tMinutes = (d / _pathIAS) * 60.0; // (nm / knots) * 60 = time in minutes
|
|
|
|
|
|
|
|
|
|
double deltaFt; // change in altitude in feet
|
|
|
|
|
if (w->flag(WPT_ARRIVAL) && !w->flag(WPT_MISS)) {
|
|
|
|
|
deltaFt = -_pathDescentFPM * tMinutes;
|
|
|
|
|
double dist = SGGeodesy::distanceM(d->waypoints[index-1].turnExitPos,
|
|
|
|
|
d->waypoints[index].turnEntryPos);
|
|
|
|
|
if (d->waypoints[index-1].flyOver) {
|
|
|
|
|
// all the turn distance counts towards this leg
|
|
|
|
|
dist += d->waypoints[index-1].turnDistanceM();
|
|
|
|
|
} else {
|
|
|
|
|
deltaFt = _pathClimbFPM * tMinutes;
|
|
|
|
|
// add half of turn distance
|
|
|
|
|
dist += d->waypoints[index-1].turnDistanceM() * 0.5;
|
|
|
|
|
}
|
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|
|
|
|
|
|
|
|
return prevAlt + deltaFt;
|
|
|
|
|
if (!d->waypoints[index].flyOver) {
|
|
|
|
|
// add half turn distance
|
|
|
|
|
dist += d->waypoints[index].turnDistanceM() * 0.5;
|
|
|
|
|
}
|
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|
|
|
|
|
|
|
|
return dist;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
double RoutePath::computeTrackForIndex(int index) const
|
|
|
|
|
double RoutePath::trackForIndex(int index) const
|
|
|
|
|
{
|
|
|
|
|
if ((index < 0) || (index >= (int) _waypts.size())) {
|
|
|
|
|
throw sg_range_exception("waypt index out of range",
|
|
|
|
|
"RoutePath::computeTrackForIndex");
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
WayptRef w = _waypts[index];
|
|
|
|
|
if (w->type() == "radialIntercept") {
|
|
|
|
|
RadialIntercept* r = (RadialIntercept*) w.get();
|
|
|
|
|
return r->courseDegMagnetic();
|
|
|
|
|
} else if (w->type() == "dmeIntercept") {
|
|
|
|
|
DMEIntercept* d = (DMEIntercept*) w.get();
|
|
|
|
|
return d->courseDegMagnetic();
|
|
|
|
|
} else if (w->type() == "hdgToAlt") {
|
|
|
|
|
HeadingToAltitude* h = (HeadingToAltitude*) w.get();
|
|
|
|
|
return h->headingDegMagnetic();
|
|
|
|
|
} else if (w->type() == "hold") {
|
|
|
|
|
Hold* h = (Hold*) w.get();
|
|
|
|
|
return h->inboundRadial();
|
|
|
|
|
} else if (w->type() == "vectors") {
|
|
|
|
|
SG_LOG(SG_NAVAID, SG_WARN, "asked for track from VECTORS");
|
|
|
|
|
throw sg_range_exception("asked for track from vectors waypt");
|
|
|
|
|
} else if (w->type() == "runway") {
|
|
|
|
|
FGRunway* rwy = static_cast<RunwayWaypt*>(w.get())->runway();
|
|
|
|
|
return rwy->headingDeg();
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
// final waypoint, use inbound course
|
|
|
|
|
if (index + 1 >= _waypts.size()) {
|
|
|
|
|
return computeTrackForIndex(index - 1);
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
// course based upon current and next pos
|
|
|
|
|
SGGeod pos, nextPos;
|
|
|
|
|
if (!computedPositionForIndex(index, pos) ||
|
|
|
|
|
!computedPositionForIndex(index + 1, nextPos))
|
|
|
|
|
{
|
|
|
|
|
SG_LOG(SG_NAVAID, SG_WARN, "unable to compute position for waypoints");
|
|
|
|
|
throw sg_range_exception("unable to compute position for waypoints");
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
return SGGeodesy::courseDeg(pos, nextPos);
|
|
|
|
|
return d->waypoints[index].legCourse;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
double RoutePath::distanceForClimb(double climbFt) const
|
|
|
|
|
double RoutePath::distanceForIndex(int index) const
|
|
|
|
|
{
|
|
|
|
|
double t = 0.0; // in seconds
|
|
|
|
|
if (climbFt > 0.0) {
|
|
|
|
|
t = (climbFt / _pathClimbFPM) * 60.0;
|
|
|
|
|
} else if (climbFt < 0.0) {
|
|
|
|
|
t = (climbFt / _pathDescentFPM) * 60.0;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
return _pathIAS * (t / 3600.0);
|
|
|
|
|
return d->waypoints[index].pathDistanceM;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
double RoutePath::magVarFor(const SGGeod& geod) const
|
|
|
|
|
double RoutePath::distanceBetweenIndices(int from, int to) const
|
|
|
|
|
{
|
|
|
|
|
double jd = globals->get_time_params()->getJD();
|
|
|
|
|
return sgGetMagVar(geod, jd) * SG_RADIANS_TO_DEGREES;
|
|
|
|
|
return d->distanceBetweenIndices(from, to);
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|